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    Laminar Boundary Layer Interaction With an Unsteady Passing Wake

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 003::page 419
    Author:
    D. E. Paxson
    ,
    R. E. Mayle
    DOI: 10.1115/1.2927891
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An investigation was conducted to study the unsteady effects of a moving wake as it passes over a laminar boundary layer in a stagnation region. Arguments are presented showing that in this region, the wake-induced unsteadiness may be treated, for the most part, as an inviscid, unsteady free stream, which impresses itself on the boundary layer flow. As a result, the boundary layer equations remain valid and, for relatively small oscillations, a solution to the equations may be obtained using standard perturbation techniques. A related experiment is then described and the results are examined in light of this analytical approach.
    keyword(s): Wakes , Boundary layers , Equations , Oscillations AND Flow (Dynamics) ,
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      Laminar Boundary Layer Interaction With an Unsteady Passing Wake

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/109383
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    contributor authorD. E. Paxson
    contributor authorR. E. Mayle
    date accessioned2017-05-08T23:36:56Z
    date available2017-05-08T23:36:56Z
    date copyrightJuly, 1991
    date issued1991
    identifier issn0889-504X
    identifier otherJOTUEI-28613#419_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/109383
    description abstractAn investigation was conducted to study the unsteady effects of a moving wake as it passes over a laminar boundary layer in a stagnation region. Arguments are presented showing that in this region, the wake-induced unsteadiness may be treated, for the most part, as an inviscid, unsteady free stream, which impresses itself on the boundary layer flow. As a result, the boundary layer equations remain valid and, for relatively small oscillations, a solution to the equations may be obtained using standard perturbation techniques. A related experiment is then described and the results are examined in light of this analytical approach.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleLaminar Boundary Layer Interaction With an Unsteady Passing Wake
    typeJournal Paper
    journal volume113
    journal issue3
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2927891
    journal fristpage419
    journal lastpage427
    identifier eissn1528-8900
    keywordsWakes
    keywordsBoundary layers
    keywordsEquations
    keywordsOscillations AND Flow (Dynamics)
    treeJournal of Turbomachinery:;1991:;volume( 113 ):;issue: 003
    contenttypeFulltext
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